中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
机构
力学研究所 [11]
采集方式
OAI收割 [11]
内容类型
期刊论文 [11]
发表日期
2025 [1]
2023 [1]
2022 [3]
2019 [1]
2018 [1]
2015 [1]
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学科主题
流体力学::实验流体... [2]
固体力学::弹性力学... [1]
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Numerical Investigation of Freestream Composition Perturbations in a Scramjet Combustor
期刊论文
OAI收割
AIAA JOURNAL, 2025, 页码: 13
作者:
Li XK(李新康)
;
Yao W(姚卫)
;
Yue LJ(岳连捷)
;
Liu QL(刘起立)
  |  
收藏
  |  
浏览/下载:23/0
  |  
提交时间:2025/10/27
Hypersonic Shock Tunnel
Scramjet Combustion Chambers
Boundary Layer Separation
Fuel Injection
Combustor Design
Fluid Mechanics
Thrust Vectoring
Numerical Simulation
Vehicle Trajectories
Partially Premixed Combustion
Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor
期刊论文
OAI收割
JOURNAL OF PROPULSION AND POWER, 2023
作者:
Wu ZJ(吴振杰)
;
Zhang QF(张启帆)
;
Yu FY(于方游)
;
Luo WH(罗苇航)
;
Gao ZB(高占彪)
  |  
收藏
  |  
浏览/下载:76/0
  |  
提交时间:2023/06/15
Scramjet Engines
Combustor Design
flame stabilization mode
transition
path dependence
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor
期刊论文
OAI收割
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11
作者:
Liu, Mingjiang
;
Sun, Mingbo
;
Zhao, Guoyan
;
Meng Y(孟宇)
;
Huang, Yuhui
  |  
收藏
  |  
浏览/下载:97/0
  |  
提交时间:2022/12/20
Tandem-cavity
Scramjet combustor
Combustion mode
Thrust performance
Investigation for Effects of Jet Scale on Flame Stabilization in Scramjet Combustor
期刊论文
OAI收割
ENERGIES, 2022, 卷号: 15, 期号: 10, 页码: 16
作者:
Li, Zhen
;
Gu, Hongbin
;
Gu HB(顾洪斌)
;
Li Z(李桢)
  |  
收藏
  |  
浏览/下载:47/0
  |  
提交时间:2022/07/18
scramjet combustor
direct-connect test
jet scale
flame stabilization
Improved delayed detached eddy simulation of supersonic combustion fueled by liquid kerosene
期刊论文
OAI收割
FUEL, 2022, 卷号: 313, 页码: 13
作者:
Shen, Wubingyi
;
Huang, Yue
;
Yao, Wei
;
Liu, Hedong
;
You, Yancheng
  |  
收藏
  |  
浏览/下载:83/0
  |  
提交时间:2022/05/17
Improved delayed detached eddy simulation
Liquid kerosene
Skeletal reaction mechanism
Equivalence ratio
Cavity-based scramjet combustor
Supersonic combustion
Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration
期刊论文
OAI收割
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: 1-8
作者:
Gu HB(顾洪斌)
;
Yue LJ(岳连捷)
;
Gao ZB(高占彪)
  |  
收藏
  |  
浏览/下载:61/0
  |  
提交时间:2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration
Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion
期刊论文
OAI收割
ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350
作者:
Yao W(姚卫)
;
Wu K(吴坤)
;
Fan XJ(范学军)
  |  
收藏
  |  
浏览/下载:65/0
  |  
提交时间:2018/12/27
Combustion Condition
Combustor Efficiency
Improved Delayed Detached Eddy Simulations
Initial Temperatures
Laminar Flame Speed
Scramjet Combustors
Supersonic Combustion
Turbulence-chemistry Interactions
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor
期刊论文
OAI收割
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
作者:
Wang ZP(王知溥)
;
Li F(李飞)
;
Gu HS
收藏
  |  
浏览/下载:65/0
  |  
提交时间:2015/06/12
Scramjet
Dual-mode combustor
Divergent angle
Cavity location
Combustion efficiency
TDLAS
Uncertainty in velocity measurement based on diode-laser absorption in nonuniform flows
期刊论文
OAI收割
APPLIED OPTICS, 2012, 卷号: 51, 期号: 20, 页码: 4788-4797
作者:
收藏
  |  
浏览/下载:61/0
  |  
提交时间:2013/01/18
Wavelength-Modulation Spectroscopy
Water-Vapor
Temperature Distributions
Scramjet Combustor
Gas Temperature
Parameters
Pressure
Sensors
A compact sensor based on near infrared absorption spectroscopy for flow diagnostics in a low density hydrogen and oxygen combustion driven shock tube
期刊论文
OAI收割
Lasers in Engineering, 2012, 卷号: 23, 期号: 1-2, 页码: 1-17
作者:
Yu XL(余西龙)
;
Li F(李飞)
;
Chen LH(陈立红)
;
Chang XY(张新宇)
收藏
  |  
浏览/下载:43/0
  |  
提交时间:2012/12/04
tunable diode-laser
water-vapor
scramjet combustor
temperature
gases
H2O
CO
oh
tunable diode laser absorption spectroscopy (tdlas)
combustion
rapid time-division-multiplexing (tdm)
temperature
water vapour concentration
low density shock tube